AVISTAR (avistar-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: AVISTAR (avistar-il) Reynolds number: 500,000 Max Cl/Cd: 81.58 at α=4.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-avistar-il-500000.txt Download as CSV file: xf-avistar-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: AVISTAR
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.000 -0.5379 0.07850 0.07582 -0.0617 1.0000 0.0365
-10.750 -0.5693 0.07231 0.06950 -0.0665 1.0000 0.0365
-10.500 -0.5981 0.06828 0.06535 -0.0673 1.0000 0.0365
-10.250 -0.6255 0.06578 0.06276 -0.0640 1.0000 0.0365
-10.000 -0.6488 0.06101 0.05791 -0.0618 0.9972 0.0367
-9.750 -0.6227 0.05719 0.05418 -0.0643 0.9949 0.0370
-9.500 -0.6045 0.05418 0.05114 -0.0664 0.9874 0.0372
-9.250 -0.5888 0.05137 0.04826 -0.0682 0.9768 0.0375
-9.000 -0.5757 0.04865 0.04542 -0.0691 0.9638 0.0379
-8.750 -0.5659 0.04617 0.04280 -0.0688 0.9491 0.0384
-8.500 -0.5437 0.03210 0.02811 -0.0642 0.9083 0.0417
-8.250 -0.5470 0.02677 0.02253 -0.0620 0.8993 0.0423
-8.000 -0.5305 0.02435 0.02012 -0.0615 0.8927 0.0427
-7.750 -0.5146 0.02249 0.01823 -0.0607 0.8860 0.0431
-7.500 -0.4994 0.02075 0.01640 -0.0596 0.8792 0.0437
-7.250 -0.4848 0.01909 0.01458 -0.0582 0.8731 0.0445
-7.000 -0.4710 0.01805 0.01317 -0.0559 0.8663 0.0473
-6.750 -0.4634 0.01518 0.00991 -0.0533 0.8597 0.0487
-6.500 -0.4428 0.01371 0.00842 -0.0528 0.8545 0.0494
-6.250 -0.4221 0.01255 0.00721 -0.0522 0.8490 0.0503
-6.000 -0.4226 0.02268 0.01632 -0.0490 0.8540 0.0407
-5.750 -0.3986 0.02097 0.01446 -0.0484 0.8486 0.0398
-5.500 -0.3736 0.01960 0.01294 -0.0478 0.8429 0.0394
-5.250 -0.3482 0.01854 0.01174 -0.0472 0.8377 0.0395
-5.000 -0.3223 0.01768 0.01076 -0.0467 0.8327 0.0397
-4.750 -0.2961 0.01703 0.01003 -0.0464 0.8268 0.0405
-4.500 -0.2699 0.01642 0.00932 -0.0459 0.8209 0.0410
-4.250 -0.2436 0.01586 0.00865 -0.0455 0.8154 0.0414
-4.000 -0.2171 0.01540 0.00815 -0.0451 0.8093 0.0417
-3.750 -0.1912 0.01447 0.00722 -0.0448 0.8032 0.0423
-3.500 -0.1663 0.01378 0.00653 -0.0442 0.7975 0.0430
-3.250 -0.1411 0.01332 0.00610 -0.0437 0.7914 0.0438
-3.000 -0.1156 0.01295 0.00573 -0.0432 0.7846 0.0450
-2.750 -0.0903 0.01262 0.00536 -0.0426 0.7783 0.0461
-2.500 -0.0649 0.01228 0.00502 -0.0420 0.7711 0.0469
-2.250 -0.0393 0.01201 0.00471 -0.0414 0.7633 0.0477
-2.000 -0.0155 0.01157 0.00424 -0.0405 0.7559 0.0487
-1.750 0.0090 0.01120 0.00389 -0.0398 0.7472 0.0501
-1.500 0.0345 0.01098 0.00363 -0.0393 0.7393 0.0520
-1.250 0.0606 0.01077 0.00342 -0.0388 0.7295 0.0540
-1.000 0.0860 0.01055 0.00314 -0.0382 0.7203 0.0560
-0.750 0.1117 0.01031 0.00291 -0.0377 0.7092 0.0590
-0.500 0.1379 0.01018 0.00273 -0.0372 0.6980 0.0625
-0.250 0.1635 0.01002 0.00254 -0.0366 0.6858 0.0703
0.000 0.1753 0.00861 0.00226 -0.0339 0.6726 0.4010
0.250 0.1863 0.00772 0.00223 -0.0304 0.6590 0.6431
0.500 0.2059 0.00750 0.00225 -0.0284 0.6443 0.7310
0.750 0.2287 0.00737 0.00225 -0.0270 0.6291 0.7842
1.000 0.2544 0.00728 0.00231 -0.0263 0.6144 0.8441
1.250 0.2850 0.00728 0.00236 -0.0267 0.6005 0.8912
1.500 0.3321 0.00732 0.00241 -0.0309 0.5873 0.9252
1.750 0.3977 0.00747 0.00251 -0.0394 0.5738 0.9418
2.250 0.4973 0.00793 0.00286 -0.0490 0.5510 0.9616
2.500 0.5350 0.00816 0.00301 -0.0511 0.5378 0.9697
2.750 0.5703 0.00839 0.00316 -0.0527 0.5244 0.9785
3.000 0.6051 0.00860 0.00332 -0.0543 0.5120 0.9881
3.250 0.6427 0.00880 0.00348 -0.0566 0.4990 0.9943
3.750 0.7176 0.00911 0.00365 -0.0612 0.4692 1.0000
4.000 0.7398 0.00921 0.00369 -0.0602 0.4527 1.0000
4.250 0.7620 0.00934 0.00376 -0.0593 0.4317 1.0000
4.500 0.7824 0.00962 0.00385 -0.0580 0.3885 1.0000
4.750 0.7919 0.01081 0.00434 -0.0551 0.2650 1.0000
5.000 0.7891 0.01303 0.00550 -0.0504 0.0707 1.0000
5.250 0.8052 0.01373 0.00606 -0.0484 0.0434 1.0000
5.500 0.8253 0.01412 0.00645 -0.0470 0.0398 1.0000
5.750 0.8451 0.01453 0.00687 -0.0455 0.0374 1.0000
6.000 0.8628 0.01508 0.00743 -0.0438 0.0356 1.0000
6.250 0.8826 0.01547 0.00784 -0.0423 0.0345 1.0000
6.500 0.9013 0.01592 0.00830 -0.0408 0.0331 1.0000
6.750 0.9187 0.01644 0.00883 -0.0390 0.0321 1.0000
7.000 0.9332 0.01711 0.00951 -0.0368 0.0313 1.0000
7.250 0.9452 0.01790 0.01033 -0.0342 0.0306 1.0000
7.500 0.9606 0.01846 0.01092 -0.0321 0.0302 1.0000
7.750 0.9736 0.01908 0.01158 -0.0297 0.0297 1.0000
8.000 0.9817 0.01972 0.01225 -0.0263 0.0293 1.0000
8.250 0.9892 0.02042 0.01298 -0.0231 0.0289 1.0000
8.500 0.9971 0.02121 0.01381 -0.0201 0.0286 1.0000
8.750 1.0057 0.02209 0.01472 -0.0175 0.0282 1.0000
9.000 1.0144 0.02305 0.01571 -0.0151 0.0279 1.0000
9.250 1.0232 0.02410 0.01678 -0.0129 0.0276 1.0000
9.500 1.0320 0.02522 0.01793 -0.0108 0.0273 1.0000
9.750 1.0403 0.02649 0.01919 -0.0088 0.0269 1.0000
10.000 1.0481 0.02797 0.02065 -0.0068 0.0265 1.0000
10.250 1.0606 0.02913 0.02184 -0.0053 0.0262 1.0000
10.500 1.0744 0.03014 0.02291 -0.0040 0.0260 1.0000
10.750 1.0887 0.03120 0.02400 -0.0028 0.0258 1.0000
11.000 1.1038 0.03226 0.02511 -0.0016 0.0256 1.0000
11.250 1.1198 0.03333 0.02622 -0.0005 0.0254 1.0000
11.500 1.1370 0.03440 0.02733 0.0005 0.0253 1.0000
11.750 1.1551 0.03548 0.02845 0.0014 0.0251 1.0000
12.000 1.1747 0.03658 0.02960 0.0022 0.0250 1.0000
12.250 1.1955 0.03774 0.03081 0.0029 0.0249 1.0000
12.500 1.2165 0.03901 0.03214 0.0036 0.0249 1.0000
12.750 1.2372 0.04040 0.03362 0.0042 0.0249 1.0000
13.000 1.2532 0.04190 0.03523 0.0051 0.0247 1.0000
13.250 1.2669 0.04352 0.03695 0.0061 0.0245 1.0000
13.500 1.2827 0.04540 0.03896 0.0070 0.0246 1.0000
13.750 1.2999 0.04762 0.04132 0.0078 0.0249 1.0000
14.000 1.3166 0.05016 0.04400 0.0084 0.0253 1.0000
14.250 1.2948 0.05619 0.05095 0.0120 0.0356 1.0000
14.500 1.2675 0.05801 0.05294 0.0168 0.0355 1.0000
14.750 1.2366 0.06017 0.05529 0.0208 0.0355 1.0000
15.000 1.2066 0.06300 0.05831 0.0238 0.0354 1.0000
15.250 1.1732 0.06640 0.06190 0.0262 0.0353 1.0000
15.500 1.1415 0.07053 0.06621 0.0277 0.0352 1.0000
15.750 1.1124 0.07499 0.07084 0.0284 0.0352 1.0000
16.000 1.0800 0.07977 0.07579 0.0286 0.0352 1.0000
16.250 1.0513 0.08462 0.08080 0.0283 0.0352 1.0000
16.500 1.0212 0.08958 0.08592 0.0275 0.0353 1.0000
16.750 0.9913 0.09425 0.09072 0.0266 0.0353 1.0000
17.000 0.9593 0.09827 0.09487 0.0257 0.0354 1.0000
17.250 0.9274 0.10318 0.09991 0.0237 0.0355 1.0000
17.500 0.8953 0.10865 0.10552 0.0210 0.0356 1.0000
17.750 0.8625 0.11467 0.11167 0.0176 0.0356 1.0000
18.000 0.8279 0.12140 0.11853 0.0134 0.0356 1.0000
18.250 0.7902 0.12920 0.12646 0.0082 0.0357 1.0000
18.500 0.7445 0.13922 0.13662 0.0014 0.0357 1.0000
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